This paper presents a study on the stability of a composite structure with a closed section. The research was carried out solely based on numerical simulations using the finite element method. ABAQUS software was used to conduct numerical simulations, which allowed to determine the values of critical loads, as well as the corresponding forms of buckling. As part of the research, the influence of composite material arrangement of layers on the stability of the structure was analyzed. The study was conducted on a composite material, which is a carbon-epoxy composite (CFRP). The obtained research results will be verified in subsequent studies by the results of experimental tests
The object of the study was a thin-walled sample made of carbon composite. The studied profile was a...
Abstract: European aircraft industry demands for reduced development and operating costs, by 20 % a...
The object of the study was a thin-walled sample made from carbon composite. The studied profile was...
The purpose of this article is to study the effect of the layup n stability and load carrying capaci...
This paper reports the results of a numerical analysis of buckling in a carbon-fibre reinforced plas...
This paper reports the results of a numerical analysis of buckling in a carbon-fibre reinforced plas...
The subject of the study was thin-walled composite structures, which were made of carbon-epoxy compo...
The object of the study was the thin-walled profile with Z-shaped cross section made of the carbon-e...
Finite element procedures for the analysis of composite structures under compressive loads (buckling...
Introduction. Composite materials are used in the construction of transport infrastructure facilitie...
This paper presents an investigation into the effect of cutout and flange reinforcement on the buckl...
This paper is devoted to the analysis of the stability and load-carrying capacity of thin-walled com...
In this paper, a numerical simulation on a new fabrication miniature composite fuselage structure- a...
European aircraft industry demands for reduced development and operating costs. Structural weight re...
European aircraft industry demands for reduced development and operating costs, by 20% and 50% in th...
The object of the study was a thin-walled sample made of carbon composite. The studied profile was a...
Abstract: European aircraft industry demands for reduced development and operating costs, by 20 % a...
The object of the study was a thin-walled sample made from carbon composite. The studied profile was...
The purpose of this article is to study the effect of the layup n stability and load carrying capaci...
This paper reports the results of a numerical analysis of buckling in a carbon-fibre reinforced plas...
This paper reports the results of a numerical analysis of buckling in a carbon-fibre reinforced plas...
The subject of the study was thin-walled composite structures, which were made of carbon-epoxy compo...
The object of the study was the thin-walled profile with Z-shaped cross section made of the carbon-e...
Finite element procedures for the analysis of composite structures under compressive loads (buckling...
Introduction. Composite materials are used in the construction of transport infrastructure facilitie...
This paper presents an investigation into the effect of cutout and flange reinforcement on the buckl...
This paper is devoted to the analysis of the stability and load-carrying capacity of thin-walled com...
In this paper, a numerical simulation on a new fabrication miniature composite fuselage structure- a...
European aircraft industry demands for reduced development and operating costs. Structural weight re...
European aircraft industry demands for reduced development and operating costs, by 20% and 50% in th...
The object of the study was a thin-walled sample made of carbon composite. The studied profile was a...
Abstract: European aircraft industry demands for reduced development and operating costs, by 20 % a...
The object of the study was a thin-walled sample made from carbon composite. The studied profile was...